Mjassischtschew / Myasishchev / Sokol M-101T Gzhel

Touring / Utility Aircraft

Mjassischtschew / Myasishchev / Sokol M-101T Gzhel, RA-15111, c/n 15-01-011 © MilanNN
Photo ©: MilanNN (Photos at airliners.net)
The Myasishchev M-101T Gzhel is a single-engine eight-seat touring and utility aircraft developed by the Russian manufacturer JSC Myasishchev Design Bureau, produced by JSC NAZ SOKOL.
Propulsion1 Turboprop Engine
Engine ModelWalter M601F-32
Engine Power559 kW750 shp
Speed341 km/h184 kts
  212 mph
Service Ceiling7.600 m24.934 ft
Range1.100 km594 NM
684 mi.
Empty Weight2.280 kg5.027 lbs
max. Takeoff Weight3.270 kg7.209 lbs
max. Landing Weight3.160 kg6.967 lbs
Wing Span13,00 m42 ft 8 in
Length9,98 m32 ft 9 in
Height3,45 m11 ft 4 in
First Flight31.03.1995
Production Statusin production
ICAO CodeM101 M17
Data for (Version)M-101T